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Discussion :: Steam Nozzles and Turbines

  1. The impulse turbine rotor efficiency will have a maximum value of 0.5 cos 2α, where α is the nozzle exit flow angle, if the

    2. A.

     Blades are equiangular
    B.

     Blade velocity coefficient is unity
    C.

     Blades are equiangular and frictionless
    D.

     Blade solidity is 0.65

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    Answer : Option C

    Explanation :

    Explanation Not Provided

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